Pulse detonation propulsion : challenges, current status, and future perspective

By G. Roy, S. Frolov, A. Borisov, D. Netzer. 2004

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Eulerian-Lagrangian modelling of detonative combustion in two-phase gas-droplet mixtures with OpenFOAM: Validations and verifications (2020, background): “Here the C− J speeds [71] are also added for comparisons, which correspond to the premixtures with fully vaporized liquid fuels.”
Rotating detonation wave propulsion: Experimental challenges, modeling, and engine concepts (2014, neutral): “PDEs have been proposed for a variety of airbreathing and rocket applications, ranging from low-speed to the hypersonic regime [57,58].”
Propulsive performance of airbreathing pulse detonation engines (2006, methodology): “These include fuel injection and mixing, repetitive detonation initiation, integration of detonation tubes with inlet and nozzle, and overall system optimization [1,2].”
On the transition pattern of the oblique detonation structure (2012, background): “In recent years, the potential application of detonation waves in hypersonic propulsion systems has been widely explored, see Kailasanath (2003) and Roy et al. (2004).”